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ADs [at] easa.europa [dot] eu
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| Number |
26-012 |
| Issued by |
Europe |
| Issue date |
2026-01-23 |
| EASA approval number |
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| ATA Chapter |
05 |
Approval Holder / Type Designation |
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2024-0080 dated 26 March 2024.
|
| Publication(s) and related information |
Airbus A330-700L ALS Part 2, DT-ALI, Revision 02 dated 19 December 2025.
The use of later approved revisions of the above-mentioned document, or of variations to the above-mentioned document which include the content of above-mentioned document, is acceptable for compliance with the requirements of this AD. |
| Remarks |
1.
This Proposed AD will be closed for consultation on 20 February 2026.
2.
Enquiries regarding this PAD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
3.
Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this PAD, and which may occur, or have occurred on a product, part or appliance not affected by this PAD, can be reported to the EU aviation safety reporting system. This may include reporting on the same or similar components, other than those covered by the design to which this PAD applies, if the same unsafe condition can exist or may develop on an aircraft with those components installed. Such components may be installed under an FAA Parts Manufacturer Approval (PMA), Supplemental Type Certificate (STC) or other modification.
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